English
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About The Book
Description
Author
This book uncovers design considerations for an inlet of a split-wing electric distributed propulsion aircraft. The purpose of this document is to demonstrate the effectiveness of the split-wing design for electric an hybrid-electric systems. It is still unknown whether the split-wing system is competitive compared to ''over-wing'' and ''under-wing'' configurations. Further investigation is required to better understand these new aircraft configurations.
Piracy-free
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*COD & Shipping Charges may apply on certain items.
Review final details at checkout.
Details
ISBN 13
9783659761461
Publication Date
-23-07-2015
Pages
-96
Weight
-142 grams
Dimensions
-150x220x5.53 mm
